Fatigue apparatus for geometrically complex non-standardized specimens

Standard Test Methods (e.g. ASTM, DIN) for materials characterization in general, and for fatigue in particular, do not contemplate specimens with complex geometries, as well as the combination of axial and in-plane bending loads in their methodologies. The present study refers to some patents and the new configuration or configurations of specimens (non-standardized by the status quo of test methods) and a device developed to induce axial and bending combined forces resultants from axial loads applied by any one test equipment (dynamic or monotonic) which possesses such limitation, towards obtaining more realistic results on the fatigue behavior, or even basic mechanical properties, from geometrically complex structures. Motivated by a specific and geometrically complex aeronautic structure (motor-cradle), non-standardized welded tubular specimens made from AISI 4130 steel were fatigue-tested at room temperature, by using a constant amplitude sinusoidal load of 20 Hz frequency, load ratio R = 0.1 with and without the above referred auxiliary fatigue apparatus. The results showed the fatigue apparatus was efficient for introducing higher stress concentration factor at the welded specimen joints, consequently reducing the fatigue strength when compared to other conditions. From the obtained results it is possible to infer that with small modifications the proposed apparatus will be capable to test a great variety of specimen configurations such as: squared tubes and plates with welded or melted junctions, as well as other materials such as aluminum, titanium, composites, polymeric, plastics, etc. © 2009 Bentham Science Publishers Ltd.

Implantes porosos de titânio puro grau 2: osseointegração em tíbias de coelho

Pós-graduação em Biopatologia Bucal - ICT

Mechanical analysis of conventional and small diameter conical implant abutments

PURPOSE. The aim of the present study was to evaluate if a smaller morse taper abutment has a negative effect on the fracture resistance of implant-abutment connections under oblique compressive loads compared to a conventional abutment MATERIALS AND METHODS. Twenty morse taper conventional abutments (4.8 mm diameter) and smaller abutments (3.8 mm diameter) were tightened (20 Ncm) to their respective implants (3.5 x 11 mm) and after a 10 minute interval, implant/abutment assemblies were subjected to static compressive test, performed in a universal test machine with 1 mm/min displacement, at 45 degrees inclination. The maximum deformation force was determined. Data were statistically analyzed by student t test. RESULTS. Maximum deformation force of 4.8 mm and 3.8 mm abutments was approximately 95.33 kgf and 95.25 kgf, respectively, but no fractures were noted after mechanical test. Statistical analysis demonstrated that the evaluated abutments were statistically similar (P=.230). CONCLUSION. Abutment measuring 3.8 mm in diameter (reduced) presented mechanical properties similar to 4.8 mm (conventional) abutments, enabling its clinical use as indicated. [J Adv Prosthodont 2012;4:158-61]

Mechanical segregation of apricot varieties and their ripeness levels at harvest

Some laboratory tests consisting on quasi-static compression and puncture forces carried out on twelve varieties of apricot during 1990 and 1991 were effective in sorting them. These mechanical properties show a high correlation w i th the ethylene production rate per fruit, so allowing to discriminate between ripeness levels at harvest. In this study it is also demonstrated that puncture seems to be the less variable mechanical test. The values (N/mm) obtained with it show a highly significant correlation with compression resistance and with quasi-static compression damage of the fruits.

Development of a test methodology for evaluating crash compatibility and aggressiveness. Test report 1: 1975 Honda Civic CVCC-to-NHTSA test device.

National Highway Traffic Safety Administration, Washington, D.C.

Development of a test methodology for evaluating crash compatibility and aggressiveness. Test report 2: 1975 Ford Torino-to-NHTSA test device.

National Highway Traffic Safety Administration, Washington, D.C.

Development of a test methodology for evaluating crash compatibility and aggressiveness. Test report 3: 1975 Volvo 244DL-to-NHTSA test device.

National Highway Traffic Safety Administration, Washington, D.C.

Development of a test methodology for evaluating crash compatibility and aggressiveness. Test report 4: 1975 Plymouth Fury-to-NHTSA test device.

National Highway Traffic Safety Administration, Washington, D.C.

Mobile parametric measurement device. Volume II: test procedures. Users manual.

National Highway Traffic Safety Administration, Washington, D.C.

Correlation of braking system defects and performance inspection. Volume II: technical report. Final report.

Mode of access: Internet.

Correlation of braking system defects and performance inspection. Volume I: summary report.

National Highway Traffic Safety Administration, Washington, D.C.

Pilot field test and evaluation center. Final report.

Federal Highway Administration, Washington, D.C.

Analytical study for evaluation of rollover test devices. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Passenger vehicle tire inspection equipment - volume I: summary. Final report.

National Highway Traffic Safety Administration, Washington, D.C.

Passenger vehicle tire inspection equipment - volume II: technical report. Final report.

National Highway Traffic Safety Administration, Washington, D.C.